ZALA 421-12
Micro air vehicle
![](http://upload.wikimedia.org/wikipedia/commons/thumb/a/ac/ZALA_421-12.jpg/200px-ZALA_421-12.jpg)
ZALA 421-12 is a micro miniature UAV developed and produced by the Izhevsk-based company ZALA Aero. It is a small, portable and reliable UAV platform. ZALA 421-12 is designed for front-line reconnaissance, overground and overseas surveillance. It takes 3 minutes to prepare ZALA for launching. The UAV is operated in the autonomous or semi-autonomous mode.
Specifications
Physical:
- Takeoff weight, kg - 3,9;
- Navigation - GNSS;
- Flight duration, h - 2;
- Engine - electric;
- Minimum speed, km/h. - 65;
- Maximum speed, km/h - 120 (limited by program);
- Maximum flight altitude, m above the sea level - 3600;
- Wingspan, m - 1,6;
- Length, m - 0,62;
- Wind speed during takeoff, no more than m/s - 10;
- Payload weight, kg max - 1;
- Launch - by means of catapult;
- Landing - parachute.
Payload:
- Color Video camera (550 TVL)
- Infrared camera (320*240 px)
- Photo camera (10 megapixels)
- Hazard Gas Analysis Module (Optional)
References
"ZALA 421-12 Russian Unmanned Aerial Vehicle (UAV)".
External links
- zala.aero: Official site.
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Aircraft produced by ZALA Aero
- 421-06
- 421-08
- 421-12
- Kub-BLA
- Lancet
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